A novel quasi-dynamic guidance law for a dynamic dual-spin projectile with non-conventional, asymmetric roll constraints

J Norris, J Economou… - Proceedings of the …, 2022 - journals.sagepub.com
A novel quasi-dynamic guidance law (QDGL) is presented for a dual-spin projectile (DSP)
with unconventional constraints on roll direction. A 7 degree-of-freedom (DOF) dynamic …

Comprehensive Evaluation of Drone Control Systems-PID vs. High-Speed Switching Controllers

AAA Alrawi, S GRAOVAC… - … Multi-Conference on …, 2024 - ieeexplore.ieee.org
The growing prevalence of Unmanned Aerial Vehicles (UAVs) in many fields has led to a
high need for sophisticated control systems to assure the best possible performance. This …

An Expanded Two-Dimensional Proportional–Derivative Command to Line-of-Sight Guidance Law

BG Penev - Gyroscopy and navigation, 2018 - Springer
This paper deals with an expanded two-dimensional (2D) proportional-derivative (PD)
command to line-of-sight (CLOS) guidance law which fights the spiral type trajectory of an …

[PDF][PDF] „Расширенное двухмерное пропорционально-дифференциальное командное наведение по линии визирования “

БГ Пенев - Гироскопия и навигация, 2018 - elektropribor.spb.ru
B статье рассматривается расширенное двухмерное (2D) пропорционально-
дифференциальное командное наведение по линии визирования, которое позволяет …

[PDF][PDF] A Simplified Adaptive Two-Dimensional Proportional–Derivative Command to Line-of-Sight Guidance Law

BG Penev - journal.iiit.bg
This paper deals with a simplified adaptive two-dimensional (2D) proportional-derivative
(PD) command to line-of-sight (CLOS) guidance law which widens the interval of stability of …

A novel dual-spin actuation mechanism for small calibre, spin stabilised, guided projectiles

JJ Norris - 2021 - dspace.lib.cranfield.ac.uk
Small calibre projectiles are spin-stabilised to increase ballistic stability, often at high
frequencies. Due to hardware limitations, conventional actuators and meth ods are unable to …

[PDF][PDF] Actuator Fault Tolerant Terminal Sliding Mode Guidance Law with Impact Angle and Acceleration Constraints

F Kırımlıoğlu, E Kutluay - 2021 - academia.edu
ABSTRACT A terminal sliding-mode guidance law is proposed in order to achieve actuator
fault tolerance and desired terminal impact angle for an anti-tank missile. Impact angle is an …